JPS5817706A - Antenna device - Google Patents

Antenna device

Info

Publication number
JPS5817706A
JPS5817706A JP11528381A JP11528381A JPS5817706A JP S5817706 A JPS5817706 A JP S5817706A JP 11528381 A JP11528381 A JP 11528381A JP 11528381 A JP11528381 A JP 11528381A JP S5817706 A JPS5817706 A JP S5817706A
Authority
JP
Japan
Prior art keywords
horn
antenna
points
distance
electric field
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP11528381A
Other languages
Japanese (ja)
Inventor
Hisao Iwasaki
久雄 岩崎
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toshiba Corp
Original Assignee
Toshiba Corp
Tokyo Shibaura Electric Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Toshiba Corp, Tokyo Shibaura Electric Co Ltd filed Critical Toshiba Corp
Priority to JP11528381A priority Critical patent/JPS5817706A/en
Publication of JPS5817706A publication Critical patent/JPS5817706A/en
Pending legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/12Supports; Mounting means
    • H01Q1/125Means for positioning

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

PURPOSE:To accurately obtain the direction of antenna radiation by ratating a primary feeding horn of a mirror surface antenna mounted on a satellite around its fitting axis and measuring the strength of electric field at least for three points on ground. CONSTITUTION:A primary power feeding horn 12 of a circular symmetrical parabola antenna 11 mounted on a satellite 10 is placed on a focus of the antenna 11. A device 13 moves the horn 12 by a minute distance d1 and the horn 12 is rotated with a device 14 in the radius. In this case, at observing points (a), (b) and (c) on ground, the strength of electric field of a radiation pattern beam- shifted due to the movement of the horn 12 by the distance d1 is measured. Next, the horn 12 is further moved by a distance d1 and similar measurement is performed. This operation is repeated by N times. Taking distances corresponding to respective measuring ponts as da, db, dc, beam shift angles thetaa, thetab, thetac corresponding to the points can be obtained. Next, by drawing circles with thetaa-thetac in shift angles with the measuring points (a-c) as the center, the point where the three circles meet is the center of direction when the horn 12 is located at the focus.

Description

【発明の詳細な説明】 本発明は、アンテナ放射指向性の指向方向測定を行なう
アンテナ装置に係シ、特に鏡面アンテナの一次給電ホー
ンの走査方法に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an antenna device for measuring the directivity of antenna radiation directivity, and more particularly to a method for scanning a primary feeding horn of a mirror antenna.

従来の指向方向を求める例として、静止衛星に4載され
たアンチjの放射指向方向を求める方法について説明す
る。
As an example of a conventional method for determining the pointing direction, a method for determining the radiation pointing direction of four anti-j mounted on a geostationary satellite will be described.

第1図に示すように、静止衛Jilに搭載されたアンテ
ナ2の地表面上3での前記アンテナ2の放射指向方向を
求めるためKは、地上の固定局4tたは、可111mア
ンテナを用いた車載局(移動局)5で電界強度を測定す
る。その地上の測定結果°を基にして、前記アンテナの
放射−向“方向を推定している。
As shown in Fig. 1, K uses a fixed station 4t on the ground or a 111m antenna to determine the radiation direction of the antenna 2 mounted on the geostationary satellite Jil above the ground surface 3. The electric field strength is measured at the vehicle-mounted station (mobile station) 5. Based on the ground measurement results, the radiation direction of the antenna is estimated.

上記の電界強度測定には、次のような問題がある。短時
間内に全測定点の電界強−を測定できないので、測定は
、長時間にわたって蒋なわれる。
The above electric field strength measurement has the following problems. Since it is not possible to measure the electric field strength at all measurement points within a short period of time, the measurement is carried out over a long period of time.

その結果測定結果の中に衛凰上の送信系の変動、また各
測定時における伝搬路のゆらぎや損失が異゛なシ天候等
の影醤が入シ込むため放射指向方向が正確に求められな
い。     ゛ 本発明は、・以上の点に鑑みてなされたもので、衛星に
搭載されたパラボラアシナナ等ゐ鏡面゛アンテナ゛の1
次給電ホ゛=ン釜、その堆り付は軸のまわシに回転させ
、少なくとも地上の3点で電界値゛度を測定するもので
ある。その測定結果か゛ら前記アンテナの放射指向方向
を正確に求めることができ。
As a result, the radiation directional direction cannot be accurately determined because the measurement results include fluctuations in the transmission system on the satellite, fluctuations in the propagation path at each measurement time, and influences such as weather, etc. do not have.゛The present invention has been made in view of the above points.
The secondary power supply horn is rotated around its axis, and the electric field value is measured at at least three points on the ground. From the measurement results, the radiation directivity direction of the antenna can be accurately determined.

る。このアンテナ装置を提供するものである。Ru. This antenna device is provided.

この一定法は、短時間で行なえるので、従来のが入シ込
壜ない。
This constant method can be performed in a short time and does not require conventional injection bottles.

以下、本発明を実施例により詳細に説明する。Hereinafter, the present invention will be explained in detail with reference to Examples.

第2図は、本発明の一実施例を示し九もので、静止衛鳳
10.円形対称パラボラアンテナ11.導波管で成シ立
っている1次給電ホー“ン12.前記給電ホーンを回転
対称軸に直交した方向に動かす装置13、前記給電ホー
ンを回転対称軸を中心として円形状に回転させる装置1
4.および地表面上の観測点15 (a)、 (b)、
 (C)から成シ立りている。
FIG. 2 shows one embodiment of the present invention. Circular symmetrical parabolic antenna 11. A primary feeding horn 12 made of a waveguide; a device 13 for moving the feeding horn in a direction perpendicular to the axis of rotational symmetry; and a device 1 for rotating the feeding horn in a circular shape around the axis of rotational symmetry.
4. and observation point 15 on the ground surface (a), (b),
It is established from (C).

本発明一実施例の具体的構成−を第3図に示す。A specific configuration of an embodiment of the present invention is shown in FIG.

第3図(1)において、円形対称パラボラ゛アンテナの
焦点加に1次給電ホーンをおくと、第3図(呻に示す実
線のアンテナ放射パターンになる。次に、第3図(1)
K示すように、1次給電ホーンを焦点の位置加からパラ
ボッアンテナの回転中心軸と直交し九方向に距離do;
A!け動かした21に置くと、第3図(呻に示す点線の
アンテナ放射パターンとなシ、実線パターンに比べて角
度0・だけビームシフトする。
In Fig. 3 (1), if the primary feeding horn is placed at the focal point of the circular symmetrical parabolic antenna, the antenna radiation pattern will be the solid line shown in Fig. 3 (1). Next, Fig. 3 (1)
As shown in K, the primary feeding horn is moved from the focal point position to the nine directions perpendicular to the rotation center axis of the parabolic antenna.
A! 21, the beam is shifted by an angle of 0° compared to the solid line antenna radiation pattern shown in FIG.

このホーンの移動1i111d・とビームシフト角0.
との間KFil対1の対応がある。
This horn movement is 1i111d and the beam shift angle is 0.
There is a KFil-to-one correspondence between .

そこで、1次給電ホーンを焦点加におき、次に第4図に
示すように装置口で微小距離d1移動し、その半径でホ
ー/12を装置14で回転させる。
Therefore, the primary feeding horn is placed in focus, and then, as shown in FIG. 4, the device mouth is moved by a minute distance d1, and the device 14 rotates the ho/12 at that radius.

このとき、地上のam点m、 b、 cにおいて、1次
給電ホーン12を距離d、動かしたことKよるビームシ
フトした放射パターンの電界強度を測定する。
At this time, at points m, b, and c on the ground, the electric field strength of the beam-shifted radiation pattern caused by moving the primary feeding horn 12 by distance d and K is measured.

次に、1次ホーンをさらに距離dt!illかし、その
半径でホーンを回転し、先と同様にa、 b、 cでさ
らにビームシフトした放射パターンの電界を測定する。
Next, move the primary horn further to a distance dt! However, rotate the horn by that radius and measure the electric field of the radiation pattern further beam-shifted at a, b, and c as before.

このことをN回繰り返す。Repeat this N times.

この測定では、1次ホーン移動距離d1を微小間隔にす
れば、必ず、測定点a、b、cにおいて、観測電界強直
が、最大となる状態がある。このときが、測定点に対し
てビーム中心が向いた状態である。
In this measurement, if the primary horn moving distance d1 is set to a minute interval, there is always a state in which the observed electric field tetanization is maximum at measurement points a, b, and c. At this time, the beam center is directed to the measurement point.

そのときの1次ホーン移動距離がわかる。それぞれの測
定点く対応した距離を’a e db * dgとする
と、これに対応し九ビー五シフト量−a e ’b *
 ’c カ求められ−る。
The primary horn movement distance at that time can be determined. If the distance corresponding to each measurement point is 'a e db * dg, then the corresponding nine bee shift amount - a e 'b *
'c is required.

第5図(→に示すように、1次ホーンを焦点においたと
きの指向中心なtとすると、とのtを中心にして、1次
ホーンを’am’b*’c動かし九ときのビームシフト
角’ae’be−6となる円を描、けば、この円の上に
必ず測定点a、 b、 cがある。
Fig.5 If you draw a circle with a shift angle 'ae'be-6, there will always be measurement points a, b, and c on this circle.

従って、第5図(&0に示すように、暑eb、cを中心
として−a−e’b*θ、となる円を描けば、3つの円
が交わる点が、1本ホーンを焦点に置い九ときの指向中
心tでToみ、。
Therefore, as shown in Figure 5 (&0), if you draw a circle with -a-e'b*θ centered on heat eb, c, the point where the three circles intersect will be the point where one horn is at the focal point. Look at the orientation center t at nine o'clock.

゛  本発明は、従来の測定方式に比べて、短時間内に
測定が行なえるので、従来方式の欠点であった送信系の
変動ま九測定時ごとの伝搬路のゆらぎや損失が入シ込ま
ないので、放射指向方向を正確に求めることが!きる。
゛ Compared to conventional measurement methods, the present invention can perform measurements in a shorter period of time, so fluctuations in the transmission system, which were disadvantages of conventional methods, and fluctuations in the propagation path and losses at each measurement time are not introduced. Therefore, it is impossible to accurately determine the radiation direction! Wear.

この測定点の数を4点以上に−すれば、さらに精度が上
がる。
If the number of measurement points is increased to four or more, the accuracy will further increase.

本発明の実施例として、円形対称パラボラアンテナを用
いたが、円形対称である必taなく、また、イ2ボ2ア
ンテナ以外の鏡面アンテナでも同様な効果が得られる。
Although a circularly symmetrical parabolic antenna is used in the embodiment of the present invention, it does not necessarily have to be circularly symmetrical, and the same effect can be obtained with a mirror antenna other than the I2BO2 antenna.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は、従来の測定方式を示す図、第2図は、本実、
羽の一実施例を示す図、第3図及び第一4図は、本発明
の具体例を示す図s pit s図は、指向中心を求め
る方法を示す図、である。 1・・・衛 星、      2・・・アンテナ、3・
・・地 表、      4・・・固 定 局、5・・
・移 動 局、10・・・衛 星、11・・・アンテナ
、     戎・・・1次ホーン、13・・・1次ホー
ンをその取シ付は軸と直交し丸方向に動かす装置、 14・・・1次ホーンを焦点を中心にして回軸させる装
置、 15・・・地 機 面、    に・・・焦 点、21
・・・1次ホーンを距離d1だけ動かした点。 代理人 弁理士  則近憲佑 (ほかl−名)第1図 τ1 第2図 第8図 (ムJ (L〕 θ=ρ   θ 第4図 第5図
Figure 1 shows the conventional measurement method, Figure 2 shows the actual measurement method,
FIGS. 3 and 4 are diagrams showing an example of the wing, and FIGS. 3 and 4 are diagrams showing a specific example of the present invention. The pit s diagram is a diagram showing a method for determining the pointing center. 1...Satellite, 2...Antenna, 3.
...Ground surface, 4...Fixed station, 5...
・Mobile station, 10... Satellite, 11... Antenna, Cap... Primary horn, 13... Device for moving the primary horn in a circular direction with its mounting perpendicular to the axis, 14 ... device for rotating the primary horn around the focal point, 15... ground plane, to... focal point, 21
...The point where the primary horn is moved by a distance d1. Agent Patent attorney Kensuke Norichika (and other names) Figure 1 τ1 Figure 2 Figure 8 (MuJ (L) θ=ρ θ Figure 4 Figure 5

Claims (1)

【特許請求の範囲】[Claims] パラボラアンテナ等の鏡面アンテナと、前記アンテナの
一次給電ホーンの取り付は軸と直交した方向に、前記−
次給電ホーンを動かす装置と、前記の取シ付は軸の囲シ
を円形状に回転させる装置とを備え、少なくとも電界強
度測定点が3力所以上有するように構成して成ることを
特徴とするアンテナ装置。
The mirror antenna such as a parabolic antenna and the primary feeding horn of the antenna are attached in a direction perpendicular to the axis.
It is characterized by comprising a device for moving the secondary power supply horn and a device for rotating the enclosure of the shaft in a circular shape, and configured to have at least three or more electric field strength measurement points. antenna device.
JP11528381A 1981-07-24 1981-07-24 Antenna device Pending JPS5817706A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11528381A JPS5817706A (en) 1981-07-24 1981-07-24 Antenna device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11528381A JPS5817706A (en) 1981-07-24 1981-07-24 Antenna device

Publications (1)

Publication Number Publication Date
JPS5817706A true JPS5817706A (en) 1983-02-02

Family

ID=14658822

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11528381A Pending JPS5817706A (en) 1981-07-24 1981-07-24 Antenna device

Country Status (1)

Country Link
JP (1) JPS5817706A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6115209A (en) * 1984-06-29 1986-01-23 Sumitomo Metal Ind Ltd Copying method of welding line
JPH04299604A (en) * 1991-03-27 1992-10-22 Honda Motor Co Ltd Antenna with reflector
FR2850795A1 (en) * 2003-01-30 2004-08-06 Thomson Licensing Sa Antenna alignment process for multimedia communication service, involves aligning antenna in center of curve described by high altitude platform, based on result of comparison between variation of residual power and threshold
GB2553302A (en) * 2016-08-30 2018-03-07 Avanti Communications Group Plc Satellite equipment

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6115209A (en) * 1984-06-29 1986-01-23 Sumitomo Metal Ind Ltd Copying method of welding line
JPH04299604A (en) * 1991-03-27 1992-10-22 Honda Motor Co Ltd Antenna with reflector
FR2850795A1 (en) * 2003-01-30 2004-08-06 Thomson Licensing Sa Antenna alignment process for multimedia communication service, involves aligning antenna in center of curve described by high altitude platform, based on result of comparison between variation of residual power and threshold
EP1605542A1 (en) * 2003-01-30 2005-12-14 Thomson Licensing Process for aligning at least one ground antenna with a platform flying at high altitude
GB2553302A (en) * 2016-08-30 2018-03-07 Avanti Communications Group Plc Satellite equipment

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